2018 IEEE/ION Position, Location and Navigation Symposium (PLANS) 2018
DOI: 10.1109/plans.2018.8373430
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ECEF position accuracy and reliability in the presence of differential correction latency

Abstract: Many applications, including connected and autonomous vehicles, would benefit from navigation technologies reliably achieving sub-meter position accuracy. Differentially corrected single frequency Global Navigation Satellite Systems (GNSS) are a suitable low cost solution. Differential corrections delivered to a roving vehicle on a nationwide scale will be subject to latency between their time-of-applicability and their time-ofreception at the vehicle. The main contribution of this article is a study of the ef… Show more

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Cited by 6 publications
(3 citation statements)
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“…Further comparison as a function of the NP-KF threshold γ and the number of measurements affected by outliers are also of interest. A companion paper at this conference [29] discusses and compares KF algorithms and a differential correction computation approach to maintain accuracy in the presence of communication latency.…”
Section: Discussionmentioning
confidence: 99%
“…Further comparison as a function of the NP-KF threshold γ and the number of measurements affected by outliers are also of interest. A companion paper at this conference [29] discusses and compares KF algorithms and a differential correction computation approach to maintain accuracy in the presence of communication latency.…”
Section: Discussionmentioning
confidence: 99%
“…In the standard position, velocity, and acceleration (PVA) model, the rover state is x=false[p,v,afalse]double-struckR9, where p , v , and a represent the rover three‐dimensional position, velocity, and acceleration vectors, respectively, local in tangent frame. The continuous‐time PVA vehicle model is ẋ(t)=0I000I00λIx(t)+00Iωa(t), where ωafalse(tfalse)double-struckR3 is modeled as a white Gaussian noise with power spectral density Qa=σa2I.…”
Section: Experiment: Models and Hardware Set Upmentioning
confidence: 99%
“…The corresponding discrete‐time PVA model is given by Equation with Φk=ITIa3I0Ia2I00a1I,Gk=000,ΓkT5false/2false/200.1emIT3false/2false/30.1emITI,andΩk=00σa20.1emI, where T represents the GPS sampling time and all submatrices are three by three with a 1 = e − λT , a 2 =(1− e − λT )/ λ , a 3 =( λT −1+ e − λT )/ λ 2 , and ωkscriptNfalse(0,0.1emnormalΩkfalse). The approximation indicated in Γ k yields the correct diagonal of the discrete‐time noise covariance matrix, but Qk=normalΓknormalΩknormalΓk and approximates the off‐diagonal terms relative to the exact calculation.…”
Section: Experiment: Models and Hardware Set Upmentioning
confidence: 99%